The V/STOL Aircraft Propulsive Effects (VAPE) computerized prediction method is evaluated. The program analyzes viscous effects, various jet, inlet, and Short TakeOff and Landing (STOL) models, and examines the aerodynamic configurations of V/STOL aircraft.


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    Title :

    Advanced Prediction Technique for the Low Speed Aerodynamics of V/STOL Aircraft. Volume 1: Technical Discussion


    Contributors:

    Publication date :

    1984


    Size :

    148 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English